Flexible Circuits for Electrical Harnesses

ABSTRACT

Provided are electrical harness assemblies and methods of forming such harness assemblies. A harness assembly comprises a conductor trace, comprising a conductor lead with a width-to-thickness ratio of at least 2. This ratio provides for a lower thickness profile and enhances heat transfer from the harness to the environment. In some examples, a conductor trace may be formed from a thin sheet of metal. The same sheet may be used to form other components of the harness. The conductor trace also comprises a connecting end, monolithic with the conductor lead. The width-to-thickness ratio of the connecting end may be less than that of the conductor trace, allowing for the connecting end to be directly mechanically and electrically connected to a connector of the harness assembly. The connecting end may be folded, shaped, slit-rearranged, and the like to reduce its width-to-thickness ratio, which may be close to 1.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application claims the benefit under 35 U.S.C. § 119(e) of USProvisional Patent Application 62/616,567, entitled: “Flexible Circuitsfor Electrical Harnesses” filed on 12 Jan. 2018 (Docket No.CLNKP010P3US), U.S. Provisional Patent Application No. 62/485,544,entitled: “FLEXIBLE CIRCUITS FOR ELECTRICAL HARNESSES” filed on 14 Apr.2017 (Docket No. CLNKP010P2US), all of which are incorporated herein byreference in their entirety for all purposes.

BACKGROUND

Electrical power and control signals are typically transmitted toindividual components of a vehicle or any other machinery or systemusing multiple wires bundled together in a harness. In a conventionalharness, each wire may have a round cross-sectional profile and may beindividually surrounded by an insulating sleeve. The cross-sectionalsize of each wire is selected based on the material and currenttransmitted by this wire. Furthermore, resistive heating and thermaldissipation is a concern during electrical power transmission requiringeven larger cross-sectional sizes of wires in a conventional harness. Asa result, harnesses can be rather bulky, heavy, and expensive tomanufacture. Yet, automotive, aerospace and other industries strive forsmaller, lighter, and less expensive components.

SUMMARY

Provided are electrical harness assemblies and methods of forming suchharness assemblies. A harness assembly comprises a conductor trace,comprising a conductor lead with a width-to-thickness ratio of at least2. This ratio provides for a lower thickness profile and enhances heattransfer from the harness to the environment. In some examples, aconductor trace may be formed from a thin sheet of metal. The same sheetmay be used to form other components of the harness. The conductor tracealso comprises a connecting end monolithic with the conductor lead. Thewidth-to-thickness ratio of the connecting end may be less than that ofthe conductor trace, allowing for the connecting end to be directlymechanically and electrically connected to a connector of the harnessassembly. The connecting end may be folded, shaped, slit-rearranged, andthe like to reduce its width-to-thickness ratio, which may be close to1.

In some embodiments, an electrical harness assembly comprises aconnector and a first conductor trace. The connector comprises a firstcontact interface and a first connecting portion. The first conductortrace comprises a first conductor lead and a first connecting end. Thefirst conductor lead and the first connecting end of the first conductortrace are monolithic. The first conductor lead has a width-to-thicknessratio of at least 2. The first connecting end of the first conductortrace electrically coupled to the first connecting portion of theconnector.

In some embodiments, the first connecting portion of the connectorcomprises a base and one or more tabs. The first connecting end of thefirst conductor trace is crimped between the base and the one or moretabs of the first connecting portion. The first connecting end of thefirst conductor trace may be welded to the base, in addition to orinstead of crimping using the tabs. The first connecting portion of theconnector comprises a first plate and a second plate parallel to thefirst plate and forming a cavity. The first connecting portion furthercomprises a biasing element protruding into the cavity from the firstplate toward the second plate. The first connecting end of the firstconductor trace protrudes into the cavity and contacts the biasingelement.

In some embodiments, the first connecting end of the first conductortrace has a width-to-thickness ratio less than the width-to-thicknessratio of the first conductor lead. The first connecting end may befolded and/or reshaped. The first connecting end may be slit into aplurality of strands, wherein the plurality of strands is bundledtogether.

In some embodiments, the electrical harness assembly further comprises asecond conductor trace, comprising a second conductor lead and a secondconnecting end. The second conductor lead and the second connecting endof the second conductor trace may be monolithic. The second conductorlead may have a width-to-thickness ratio of at least 0.5. The thicknessof the second conductor lead and the thickness of the first conductorlead are approximately equal. The second conductor lead and the firstconductor lead do not contact each other.

In some embodiments, the second connecting end of the second conductortrace is electrically coupled to multiple connecting portions of theconnector. The connector may comprise one or more jumpers electricallycoupling the multiple connecting portions. The second conductor lead maybe wider than the first conductor lead. In some embodiments, the firstconnecting end is a stack of multiple layers formed by folding the firstconductor trace. The first connecting end is a stack of two layers.

Also provided is a car door assembly, comprising a car door and anelectrical harness assembly. The car door comprises a surface. Anelectrical harness assembly directly interfaces the surface of the cardoor. The electrical harness assembly is attached to the surface of thecar door. The electrical harness assembly may be conformal to thesurface of the car door over at least 50% of the area of the electricalharness assembly. The electrical harness assembly may be attached to thesurface of the car door along at least 50% of an interface between theelectrical harness assembly and the surface of the car door.

In some embodiments, the electrical harness assembly comprises a firstinsulator, a first conductor trace, and a second insulator. The firstconductor trace is disposed between the first insulator and the secondinsulator. The first insulator is disposed between the first conductortrace and the surface of the car door. The first insulator may beadhered to the surface of the car door using a thermally conductivemounting adhesive. The thermally conductive mounting adhesive may be athermally conductive pressure-sensitive adhesive (PSA) film. The firstinsulator may comprise a material selected from the group consisting ofpolyimide (PI), polyethylene naphthalate (PEN), polyethyleneterephthalate (PET), polymethyl methacrylate (PMMA), ethyl vinyl acetate(EVA), polyethylene (PE), polypropylene (PP), polyvinyl fluoride (PVF),polyamide (PA), soldermask, and polyvinyl butyral (PVB).

These and other embodiments are described further below with referenceto the figures.

BRIEF DESCRIPTION OF THE DRAWINGS

FIGS. 1A and 1B illustrate an electrical connector assembly, inaccordance with some embodiments.

FIGS. 2A-2C illustrate an example of forming a connecting end of aconductor trace.

FIGS. 3A-3C illustrate another example of forming a connecting end of aconductor trace.

FIG. 4A illustrates an example of a partially assembled electricalharness assembly having different portions that are ready to be foldedand stacked together.

FIG. 4B illustrates an expanded view of a portion of the electricalharness assembly shown in FIG. 4A.

FIG. 5 illustrates an example of a connecting portion of a connectorcoupled to a conductor trace using a biasing element disposed in acavity of the connecting portion.

FIG. 6 is a top schematic view of a conductor trace, in accordance withsome embodiments.

FIGS. 7A and 7B are cross-sectional schematic views of different partsof the conductor trace shown in FIG. 6, in accordance with someembodiments.

FIGS. 8A-8C illustrate an example of folding a connecting end of aconductor trace.

FIGS. 9A-9C illustrate an example of shaping a connecting end of aconductor trace.

FIGS. 10A-10C illustrate an example of slitting and bundling individualstrands of a connecting end of a conductor trace.

FIG. 11A is a schematic top view of a conductor trace prior to foldingits connecting end and attaching a terminal, in accordance with someembodiments.

FIG. 11B illustrates a schematic cross-sectional view of the attachmentportion of the conductor trace shown in FIG. 11A.

FIG. 11C is a schematic top view of the conductor trace shown in FIG.11A after folding its connecting end, in accordance with someembodiments.

FIG. 11D illustrates a schematic cross-sectional view of the attachmentportion of the conductor trace shown in FIG. 11C.

FIG. 11E illustrates a schematic top view of the conductor trace shownin FIGS. 11A and 11C after attaching the terminal, in accordance withsome embodiments.

FIGS. 12A-12C illustrate schematic top views of different examples of aconductor trace prior to folding its connecting end, in accordance withsome embodiments.

FIGS. 13A-13E illustrate schematic cross-sectional views of theattachment portion of the conductor trace after folding its connectingend, in accordance with some embodiments.

FIG. 14A illustrates a schematic top view of four conductor traces priorto folding and repositioning their connecting ends and attachingterminals, in accordance with some embodiments.

FIG. 14B illustrates a schematic top view of the four conductor tracesshown in FIG. 14A after folding and repositioning their connecting endsand attaching terminals, in accordance with some embodiments.

FIG. 14C illustrates a schematic top view of conductor traces positionedout of plane and forming connections to terminals of the connector atdifferent levels.

FIGS. 14D and 14E illustrate a schematic top view of three conductortraces before and after connecting these conductor traces to terminals.

FIG. 15A illustrates a schematic top view of conductor traces withpartially formed connecting ends.

FIG. 15B illustrates a schematic top view of the conductor traces ofFIG. 15A now with fully formed connecting ends.

FIG. 16A illustrates a schematic top view of a harness assemblycomprising an insulator and multiple conductor leads adhered to andsupported by the insulator.

FIG. 16B illustrates a schematic top view of an insulator comprisingthree insulator openings that divide the insulator into four insulatorstrips.

FIG. 16C illustrates a schematic top view of the insulator shown in FIG.16B with one end of the insulator turned 90° relative to the other endwithin a plane.

FIGS. 16E and 16F illustrate schematic cross-section views of theinsulator strips of the insulator shown in FIG. 16C at differentlocations.

FIG. 17 is a process flowchart corresponding to a method of forming theinterconnect circuit, in accordance with some embodiments.

FIGS. 18A-18C illustrate a schematic top view of an electrical harnessassembly with a connector assembly with and without jumpersinterconnecting different conductor traces of the harness assembly.

FIG. 18D illustrates a schematic cross-section view of the connectorassembly shown in FIG. 18C showing arrangement of multiple jumpersinterconnecting different conductor traces of the harness assembly.

FIG. 19A illustrates a car door assembly comprising a car door and anelectrical harness assembly mechanically supported by and thermallycoupled to the car door, in accordance with some embodiments.

FIGS. 19B and 19C illustrate an electrical harness assembly beingsubstantially conformal to the surface of the door.

FIG. 20 illustrates various heat transfer aspects between a flat wire ofthe electrical harness assembly and the car door.

FIGS. 21A and 21B are schematic top and cross-section views showing thewidths of gaps between two-conductor leads.

FIGS. 22A and 22B are schematic cross-section views of a conductor traceshowing a base sublayer and two examples of a surface sublayer.

FIG. 22C is a schematic cross-section view of a conductor trace showinga base sublayer and an electrically insulating coating.

FIG. 23 illustrates an example of two harnesses supported on the samecarrier film.

DETAILED DESCRIPTION

In the following description, numerous specific details are set forth inorder to provide a thorough understanding of the presented concepts. Thepresented concepts may be practiced without some or all of thesespecific details. In other instances, well known process operations havenot been described in detail so as to not unnecessarily obscure thedescribed concepts. While some concepts will be described in conjunctionwith the specific embodiments, it will be understood that theseembodiments are not intended to be limiting.

Introduction

Electrical harnesses are used to deliver power and/or signals in variousapplications, such as vehicles, appliances, electronics, and the like.Conventional harnesses typically utilize round wires formed from roundconductive leads (e.g., solid round wires or stranded bundles of roundwires) insulated by polymer shells. These round wires are often bundledtogether into a harness. Unfortunately, these bundles can be hard tofeed through narrow spaces. Furthermore, round wires have poor thermalconnections to surrounding flat structures and therefore experience verylittle heat dissipation during their operation. As a result, largergauge wires are often used in such harnesses to avoid excessiveresistive (joule) heating. This wire oversizing, in turn, adds to thesize, weight, and cost of a harness, all of which are not desirable.

Provided are harnesses formed using flat conductor traces, rather thanwires with round cross-sections. These conductor traces may be formed,for example, from a sheet of foil. In some embodiments, all traces ofthe same harness may be formed from the same sheet of foil, therebysimplifying production of the harness and allowing for robust electricalconnections between traces due to the monolithic nature of the sheet. Inthese embodiments, the formed traces may have a coplanar orientation or,more generally, the traces may be arranged as a one-dimensional array insome cross-sections of the harness. A combination of the flat conductortraces and their arrangement allows forming a harness that is both thinand flexible as well as capable of thermal coupling to surroundingstructures. The thickness of the harness may be a combination ofthicknesses of the conductor traces, one or two insulators, and one ormore adhesive layers, if used. A thin harness or, more specifically, athin, flexible harness can be fed through narrow spaces that may be notsuitable for bundled conventional harnesses.

Because of the small overall thickness and the coplanar orientation ofthe conductor traces, the harness can be very flexible in at least adirection perpendicular to the plane of the harness. The flexibility maybe a lot greater than that of a harness formed by the bundled wires.This flexibility may be used to conform the harness to various planarand non-planar surfaces, such as an interior surface of a car door whichhas many topographical variations. For example, the electrical harnessassembly may be conformal to the surface of the car door over at least50% of the area of the electrical harness assembly or, morespecifically, at least 75% of the area o even at least 90% of the area.

Finally, the conformality and small thickness of the thin flexibleharness allows for substantial cooling of individual conductor traces inthe harness. As a result, the conductor traces with smallercross-sectional areas may be used in the provided harness than inconventional harnesses. This thermal coupling and small wirecross-section, in turn, leads to a smaller weight, size, and cost of theharnesses.

Forming Connections to Flat Conductor Traces

One challenge with using flat conductor traces in a harness is formingelectrical connections between such traces and other components, such asconnectors and other traces/wires, which may have different dimensionsor, more specifically, smaller width-to-thickness ratios. For example,connectors for wire harnesses may use contact interfaces that are squareor round, or, more generally, have comparable widths and thicknesses(e.g., have a width-to-thickness ratio of about 1 or between 0.5 and 2).On the other hand, a conductor trace in a proposed flexible circuit mayhave a width-to-thickness ratio of at least about 2 or at least about 5or even at least about 10. Such conductor traces may be referred to asflat conductor traces or flat wires to distinguish them from roundwires. Various approaches are described herein to form electricalconnections to the flat conductor traces.

FIGS. 1A and 1B illustrate electrical connector assembly 90, inaccordance with some embodiments. Electrical connector assembly 90 maybe a part of electrical harness assembly 100 further described below.Electrical connector assembly 90 comprises connector 110 and conductortrace 140 a, which may also be referred to as first conductor trace 140a to distinguish from other conductor traces of the same harness, ifpresent. For simplicity, only one conductor trace is shown in thesefigures. However, one having ordinary skill in the art would understandthat this and other examples are applicable to harnesses and connectorassemblies with any number of conductor traces.

Connector 110 comprises first contact interface 120 a and firstconnecting portion 130 a. First contact interface 120 a may be used tomake an external connection formed by connector assembly 90 and may bein the form of a pin, socket, tab, and the like. First contact interface120 a and first connecting portion 130 a may be made from the samematerials (e.g., copper, aluminum, and the like). In some embodiments,first contact interface 120 a and first connecting portion 130 a aremonolithic. For example, first contact interface 120 a and firstconnecting portion 130 a may be formed from the same strip of metal.

First conductor trace 140 a comprises first conductor lead 150 a andfirst connecting end 160 a. First connecting end 160 a is electricallycoupled to first connecting portion 130 a of connector 110.Specifically, first connecting end 160 a and first connecting portion130 a may directly contact each other and overlap within the housing ofconnector 110.

In some embodiments, each connector is coupled to a different conductortrace. Alternatively, multiple connectors may be coupled to the sameconductor trace. Furthermore, a single connector may be coupled tomultiple conductor traces. Finally, multiple connectors may be coupledto multiple conductor traces such that all of these connectors andtraces are electrically interconnected.

First conductor lead 150 a extends away from connector 110, e.g., toanother connector or forms some other electrical connection withinconnector assembly 90. The length of first conductor lead 150 a may beat least about 100 millimeters, at least about 500 millimeters, or evenat least about 3000 millimeters. First conductor lead 150 a may beinsulated on one or both sides using, for example, first insulator 142and second insulator 144 as schematically shown in FIG. 20 and describedbelow. In some embodiments, first insulator 142 and second insulator 144do not extend to first connecting end 160 a, allowing first connectingend 160 a to directly interface first connecting portion 130 a.Alternatively, one of first insulator 142 and second insulator 144 mayoverlap with first connecting portion 130 a, while still exposinganother side of first connecting end 160 a and allowing this side todirectly interface first connecting portion 130 a. In some embodiments,electrical connections to first connecting portion 130 a are madethrough openings in one of first insulator 142 and second insulator 144.In these embodiments, first insulator 142 and second insulator 144 mayoverlap with first connecting portion 130 a. In further embodiments,external insulation to first connecting end 160 a may be provided byconnector 110 or by a pottant or encapsulant surrounding firstconnecting end 160 a.

As shown in FIGS. 1A and 1B, both first conductor lead 150 a and firstconnecting end 160 a have the same thickness (e.g., formed from the samemetal sheet). First connecting end 160 a may have a width-to-thicknessratio of at least 0.5 or, more specifically, at least about 2 or even atleast about 5 or even at least about 10. The width-to-thickness ratio offirst conductor lead 150 a may be the same or different.

In some embodiments, first connecting portion 130 a of connector 110comprises base 132 and one or more tabs 134. Specifically, FIG. 1Billustrates four tabs 134 extending from base 132 (two from each side ofbase 132). However, any number of tabs can be used. First connecting end160 a of first conductor trace 140 a is crimped between base 132 andtabs 134. The crimping provides electrical connection and mechanicalcoupling between connecting portion 130 a and first connecting end 160a. The mechanical coupling helps to ensure that the electrical couplingis retained during operation of electrical harness assembly 100. Forexample, the connection between first connecting portion 130 a and firstconnecting end 160 a may be subject to mechanical stresses, creeping ofthe material (e.g., when one or both materials comprises aluminum), andthe like. Furthermore, the mechanical coupling may be used to supportfirst connecting end 160 a of first conductor trace 140 a by connector110.

In some embodiments, first connecting end 160 a of first conductor trace140 a is also welded or otherwise additionally connected to base 132 as,for example, schematically shown at locations 133 in FIGS. 1A and 1B.This connection may be carried out using various means, including butnot limited to ultrasonic welding, laser welding, resistance welding,brazing, or soldering. This connection helps form a low-resistance,stable electrical contact between first connecting end 160 a andinterfacing base 132, and may be referred to as a primary electricalconnection to distinguish from the electrical connection provided by adirect interface between connector 110 and first conductor trace 140 a.This primary electrical connection may comprise an intermix of materialsof first connecting end 160 a and interfacing base 132 and form a localmonolithic structure at each location 133. Therefore, if surfaceoxidation or other changes in surface conditions of first connecting end160 a and interfacing base 132 happen later, these changes will notimpact this primary electrical coupling between first connecting end 160a and interfacing base 132.

In some embodiments, for example in cases in which each of conductortraces 140 is not sufficiently thick to form such connections, multipleconductor traces 140 may be stacked together and this stack is coupledto connecting portion 130 of connector 110. Referring to FIGS. 2A-2B,first conductor trace 140 a and second conductor trace 140 b are foldedto form stack 151. Connector 110 is then coupled to stack 151 as shownin FIG. 2C. FIGS. 3A-3C show a different folding pattern, which alsoresults in first conductor trace 140 a and second conductor trace 140 b.While these examples (in FIGS. 2A-3C) shows a stacked form by twoconductor traces, one having ordinary skill in the art would understandthat any number of conductor traces may be stacked together by foldingor other means. Furthermore, FIGS. 2A-2B and FIGS. 3A-3C illustratefirst conductor trace 140 a and second conductor trace 140 b beingjoined together away from connector 110. Alternatively, first conductortrace 140 a and second conductor trace 140 b may be completely disjoinedaway from connector 110 and form an electrical connection only atconnector 110. Furthermore, in some examples, first conductor trace 140a and second conductor trace 140 b may remain electrically insulatedfrom each other and may be coupled to different rows of a connector ordifferent connectors altogether as, further described below withreference to FIGS. 14A-C.

FIG. 4A illustrates an example of electrical harness assembly 100, whichis only partially assembled and does not have connectors attached to itsconductor traces. Electrical harness assembly 100 comprises differentportions 101 a-101 d, used for attachment of connectors. Prior to thisattachment, various combinations of these different portions 101 a-101 dmay be stacked together in a way similar to the one described above withreference to FIGS. 2A-2B and FIGS. 3A-3C. For example, portion 101 a maybe stacked with portion 101 b such that multiple conductor traces 140a-140 c of portion 101 a (shown in FIG. 4B) overlap with correspondingconductor traces of portion 101 b. In a similar manner, portion 101 c isready to be stacked with portion 101 d such that their correspondingconductor traces overlap. For example, portions 101 a and 101 b may befolded towards each other and inserted into a single connector that isable to accept and make connections to two or more rows of conductortraces. In the latter example, to prevent the conductor traces ofportion 101 a from inadvertently contacting portion 101 b near theconnector, an insulating layer may be placed in between the two portions101 a and 101 b. Alternatively, portions 101 a-101 d or similar portionsmay be folded in such a way that an insulating layer, which may be alsoreferred to as a base layer, is stacked in conductor traces on eachfolded end. In other words, the conductor traces remain electricallyinsulated even when stacked.

Referring to FIG. 5 illustrates one example of illustrate electricalconnector assembly 90, first connecting portion 130 a of connector 110comprises first plate 135 and second plate 137 parallel to first plate135 and forming cavity 136. First connecting portion 130 a furthercomprises biasing element 138 protruding into cavity 136 from firstplate 135 to second plate 137. First connecting end 160 a of firstconductor trace 140 a protrudes into cavity 136 and contacts biasingelement 138. Biasing element 138 maintains contact with first connectingend 160 a even if first connecting end 160 a starts changing its shape(e.g., creep). Biasing element 138 may be a spring or, morespecifically, a set of springs, such as leaf springs. Alternatively,connector 110, in its entirety, may be spring loaded or may be formed sothat connector 110 compresses against first connecting end 160 a whenfirst connecting end 160 a is inserted into connector 110.

Referring to FIGS. 6 and 7A-7B, first connecting end 160 a of firstconductor trace 140 a may have a width-to-thickness ratio different thanthe width-to-thickness ratio of first conductor lead 150 a. For example,first conductor lead 150 a may be a foil strip, while first connectingend 160 a may be patterned or formed into some other shape (e.g., fromthe same foil strip). Different width-to-thickness ratios allow firstconnecting end 160 a to form robust electrical and mechanicalconnections to a connector and, at the same time, allow first conductorlead 150 a to maintain a low thickness profile away from the connector.

Different width-to-thickness ratios of first connecting end 160 a andfirst conductor lead 150 a may be achieved in various ways. For example,first connecting end 160 a may be folded, as for example, schematicallyshown in FIGS. 8A-8C. In another example, first connecting end 160 a maybe reshaped, as for example, schematically shown in FIGS. 9A-9C. In yetanother example, first connecting end 160 a may be slit into a pluralityof strands, which are bundled together, for example, as schematicallyshown in FIGS. 10A-10C. As such, first connecting end 160 a may start asfoil strip 160 a″ that goes through an intermediate shaping stage 160 a′before being formed into first connecting end 160 a.

FOLDING EXAMPLES

FIG. 11A is a schematic top view of conductor trace 140, comprisingconductor lead 150 and connecting end 160, prior to folding connectingend 160 and attaching terminal 111 (not shown) to connecting end 160.Terminal 111 may be a part of a connector described above or the entireconnector. In this example, connecting end 160 comprises attachmentportion 162, fold portion 164, and transition portion 166, such thattransition portion 166 is between conductor lead 150 and fold portion164, while fold portion 164 is positioned between attachment portion 162and transition portion 166. Fold portion 164 and transition portion 166are optional. In some examples, conductor lead 150 interfaces directlywith attachment portion 162. Alternatively, one of fold portion 164 andtransition portion 166 is positioned between conductor lead 150 andattachment portion 162.

Attachment portion 162 comprises multiple strands 161, which may beformed by slitting a metal sheet. FIG. 11B illustrates a schematiccross-sectional view of attachment portion 162 prior to its folding.Strands 161 may be coplanar at this stage.

Overall, conductor lead 150 and connecting end 160 may be monolithic(e.g., formed from the same sheet of metal). All components ofconnecting end 160, which may be attachment portion 162, fold portion164, and transition portion 166 (in this example) are also monolithic.Various processing techniques may be used to form each of theseportions, such as slitting, die cutting, laser cutting, waterjetcutting, or stamping.

The cross-sectional shape of at least attachment portion 162 and, insome embodiments, the cross-sectional shapes of fold portion 164 andtransition portion 166, change during folding of connecting end 160 as,for example, schematically shown in FIGS. 11C and 11D. Specifically,attachment portion 162 is reshaped into a bundle that has a smallerwidth-to-thickness ratio than attachment portion 162 prior to folding.More specifically, strands 161 are rearranged from their originalcoplanar shape to a new arrangement. In should be noted that whileconnecting end 160 is folded, conductor lead 150 remains substantiallythe same. Once connecting end 160 is folded, terminal 111 may beattached (e.g., crimped) to attachment portion 162 as, for example,schematically shown in FIG. 11E. Various other attachment techniques(e.g., welding, soldering) are also within the scope.

Attachment portion 162 directly interfaces and overlaps with terminal111 as, for example, schematically shown in FIG. 11E. Prior to folding,attachment portion 162 comprises multiple strands 161, separated byslits and/or gaps as, for example, shown in FIGS. 11A and 11B. Forpurposes of this disclosure, a slit is defined as a separation betweentwo adjacent strands that has zero or minimal width but allows thesestrands to move out of plane with respect to each other. Gaps have ameasurable width and are usually formed by removal of material whileforming strands 161. FIGS. 11A and 11B illustrate six strands 161forming attachment portion 162; however, any number of strands 161 iswithin the scope (two, three, four, ten, twenty, etc.). In this example,all strands 161 have the same width (W_(S)), and gaps between any pairof adjacent strands 161 have the same width (W_(T)) and are separated bythe same gap. However, as further described below with reference toFIGS. 13A-13D, strands 161 may have different widths and/or gaps.Various combinations of widths and/or gaps may be used to ensure tighterpacking in the bundle. The total width (W_(T)) of attachment portion 162is a combination of all widths of strands and all widths of gaps, ifsuch gaps are present. W_(S) and W_(T) may be chosen such that the totalcross-sectional area of the conductor material in attachment portion 162is greater than the cross-sectional area of conductor lead 150, forexample, to account for generally poorer heat dissipation of a strandedwire shape relative to a flat conductor.

When fold portion 164 is present, it extends to terminal 111 but doesnot overlap with terminal 111. Fold portion 164 may also comprisestrands 161 or parts thereof. However, when conductor trace 140 isfolded, portions of strands 161 have different arrangements in foldportion 164 and in attachment portion 162. Specifically, the portion ofstrands 161 in fold portion 164 may be twisted and/or folded to providetransition to the arrangement of strands in attachment portion 162. Theportion of strands 161 in attachment portion 162 may be substantiallyparallel to each other (e.g., aligned along the center axis extending inthe X direction). This parallel arrangement in attachment portion 162allows applying large crimping forces to attachment portion 162 withoutbraking strands 161, which in turn preserves mechanical integrity andcontinuity of strands 161. Furthermore, this parallel arrangement allowsforming a bundle with a uniform cross-section (along the center axis),which in turn provides the maximum interface area with terminal 111. Inother words, bumps and other protrusions associated with twisting andfolding are avoided in attachment portion 162.

Transition portion 166 may or may not have individual strands, gaps, orslits. Transition portion 166 may be positioned between conductor lead150 and fold portion 164 and used to transition from a smaller width ofconductor lead 150 (W_(L)) to a much larger width (W_(T)) of foldportion 164. Transition portion 166 effectively allows protecting rootedends of strands 161 from stresses. Transition portion 166 may be alsopartially folded. However, the degree of folding may be less than thatof fold portion 164.

FIGS. 12A and 12B illustrate two examples of conductor traces 140 withstrands 161 having different lengths. As described above, strands 161are folded from their initial coplanar arrangement (e.g., shown in FIGS.12A and 12B as well as FIGS. 11A and 11B) to a different (bundled) shape(e.g., shown in FIGS. 11C and 11D). This folding is used to accommodateterminal 111, which typically has a smaller width-to-thickness ratiothan strands 161 in their initial unfolded state. The folding processinvolves bringing strands 161 closer to center axis 141 of conductortrace 140. However, some strands 161 are further away from center axis141 and need to be folded more than strands 161 that are closer tocenter axis 141. To accommodate this difference in folding distances,strands 161 that are further away from center axis 141 may be longerthan strands 161 that are closer to center axis 141. This lengthdifference may be provided by different curvatures of strands 161 as,for example, shown in FIG. 12A. In this example, the projection ofstrands 161 onto center axis 141 may be substantially the same.Furthermore, the free ends of strands 161 may be substantially coplanar.For purposes of this disclosure, the term “substantially coplanar” isdefined as deviation from a common plane of less than 5 millimeters oreven less than 2 millimeters. It should be noted that the free ends ofstrands 161 may remain substantially coplanar during and after folding.

FIG. 12B illustrates another example in which all strands are straightand/or substantially parallel to center axis 141 in their initialflat/before folding shape. For purposes of this disclosure, the term“substantially parallel” is defined as angular difference of less than10° or even less than 5°. In this example, the free ends of strands 161are not coplanar before folding. However, after folding, the free endsof strands 161 may be substantially coplanar.

In some embodiments, when the free ends of strands 161 are notsubstantially coplanar after folding, these free ends may be trimmed toensure that newly formed ends (i.e., trimmed ends) are substantiallycoplanar. However, various features of conductor traces 140 describedabove may be used to yield substantially coplanar free ends of strands161 after folding of conductor traces 140 without a need for trimming.Alternatively, a trimming operation may be used in conjunction with oneor both features described above with reference to FIGS. 12A and 12B.

FIG. 12C illustrates an example of conductor trace 140 in which gaps 163between strands 161 terminate with stress relief features 165. Stressrelief features 165 may be free from sharp corners (e.g., corners with acurvature radius of less than 1 millimeter). For example, stress relieffeatures 165 may have a circular profile and may have a minimum radiusof at least 2 millimeters or even at least 5 millimeters. Elimination ofthe sharp corners allows reducing stress concentration points whilefolding and after folding of conductor trace 140. For example, strands161 may be bent, twisted, and/or folded around center axis 141 whileconductor lead 150 remains flat.

FIGS. 13A-13D illustrate different examples of bundles formed by strands161 in attachment portion 162. Strands 161 are specifically formed andfolded to fill cross-sectional profile 167, which has a circular profilein this example. It should be noted that, in some examples, strands 161are formed from the same sheet of metal and, as such, have the samethickness. The width of strands 161 and, as a result, thewidth-thickness ratios, may be the same or different. Controlling thenumber of strands 161, the width of each strand 161, and the foldedorientation of each strand 161 may be used to achieve different fillingratios, which may be higher than, for example, is possible with roundwires 161′ shown in FIG. 13E, as reference. For purposes of thisdisclosure, the filling ratio is defined as a sum of all cross-sectionalareas of strands 161 divided by the area of cross-sectional profile 167.In some embodiments, this filling ratio is at least about 80% or even atleast about 90%.

FIG. 13A illustrates an example of a bundle formed by strands 161, whichall have the same rectangular cross-sectional profile. Furthermore, theorientations of these rectangular cross-sectional profiles are the same(e.g., all long side are parallel to each other). FIG. 13B illustratesan example of a bundle formed by strands 161 all having the same squarecross-sectional profile.

FIG. 13C illustrates an example of a bundle formed by strands 161 havingboth rectangular and square cross-sectional profiles. While only twotypes of profiles are shown in this example, one having ordinary skillin the art would understand that any number of different cross-sectionalprofiles may be used in the same bundle. For example, all strands 161,forming the same bundle, may have different widths. FIG. 13D illustratesanother example of a bundle formed by strands 161 all having the samerectangular cross-sectional profile. However, unlike the example shownin FIG. 13A, the orientations of these rectangular-cross-sectionprofiles differ. For example, some strands 161 are turned 90° relativeto other strands. Any degree of rotation of the strands 161 is withinthe scope.

FIGS. 14A and 14B illustrate four conductor traces 140 before and afterconnecting these conductor traces 140 to terminals 111. Folding ofconnecting ends 160 and crimping of terminals 111 to these connectingends 160 are described above with reference to FIGS. 11A-11E. In someembodiments, the position of terminals 111 as determined by their finallocations within a connector may be different from the positions ofcenter axes 141 of individual connecting ends 160. Referring to FIGS.14A and 14B, center axes 141 of individual connecting ends 160 arespaced apart more than terminals 111. This larger spacing may be due toconnecting ends 160 being formed from the same metal sheet, whileterminals 111 may have to be positioned in the same compact connector.To accommodate this difference, conductor leads 150 may be folded toalign their connecting ends 160 with respective terminals 111.

As shown in FIG. 14B, in some embodiments, folding of conductor leads150 may cause one or more conductor leads to overlap. However, conductortraces 140, which are generally insulated (e.g., covered in aninsulation shell or positioned between insulating layers) away fromconnecting ends 160, may remain electrically insulated when theirconductor leads 150 overlap. For example, conductor leads 150 may beinsulated at the overlap location (e.g., one or more insulator layersmay be positioned between two overlapping conductor leads 150).Furthermore, as shown in FIG. 14C, conductor traces 140 may bepositioned out of plane (in the Z direction) and form connections todifferent terminals of connector 110 at different levels (spread in theZ-direction). For example, first conductor trace 140 a extends abovesecond conductor trace 140 b, third conductor trace 140 c, and fourthconductor trace 140 d, and forms a connection to a different (higher)level of connector 110. Furthermore, FIG. 14C illustrates the ability ofconductor traces 140 to cross in other directions (in the Y direction).In this example, first conductor trace 140 a crosses over (in the Ydirection) second conductor trace 140 b and third conductor trace 140 cand forms a connection roughly above fourth conductor trace 140 d. Thisfeature may provide an extra degree of freedom in terms of routingsignals from one module to another within a vehicle or any other type ofa device.

FIGS. 14D and 14E illustrate three conductor traces 140 a-140 c beforeand after connecting these conductor traces 140 a-140 c to terminals 111a-111 c. Prior to connecting these conductor traces 140 a-140 c toterminals 111 a-111 c, conductor traces 140 a-140 c may extend within abendable plane (e.g., defined by insulator 142 or a temporary liner).Insulator 142 may be also referred to as first insulator 142 whenadditional insulators (e.g., second insulator 144) are present. However,spacing between first connecting end 160 a and third connecting end 160c (within the X-Z cross-section) may not be sufficient to accommodateconnecting end 160 b. As a result, connecting end 160 b is formed in apre-folded state and positioned between first conductor lead 150 a andthird conductor lead 150 c as shown in FIG. 14D. When first connectingend 160 a and third connecting end 160 c are connected to theirrespective terminals 111 a and 111 c, more space is available in betweenthese connecting ends 160 a and 160 c and connecting end 160 b can nowbe accommodated, at least in the folded state, as shown in FIG. 14E.

FIG. 15A illustrates conductor traces 140 with partially formedconnecting ends 160. In this example, strands 161 do not have free ends.This feature simplifies handling of connecting ends 160, in particulartransferring conductor traces 140 from one supporting substrate toanother, folding connecting ends 160, and/or performing otheroperations. At this stage, strands 161 supported by bridging part 169.Bridging part 169 may be removed before or after folding connecting ends160.

FIG. 15B illustrates an example of hybrid conductor traces 140, whichinclude one conductor lead 150 and two connecting ends 160 a and 160 b.For example, one connecting end 160 a may be used for power transmission(and rated for a higher current) while another connecting end 160 b maybe used for signal (and rated for a smaller current). The size of eachconnecting end is selected for these current ratings and to accommodatecorresponding connector terminals.

FIG. 16A illustrates electrical harness assembly 100 comprisinginsulator 142 and multiple conductor leads 150 a-150 c adhered to andsupported by insulator 142. Insulator 142 comprises different insulatoropenings 143 a-143 c that allow for manipulation of insulator 142 andcorresponding conductor leads 150 a-150 c. For example, insulatoropening 143 c extends to one edge of insulator 142 and defines firstharness portion 103 a and second harness portion 103 b that can bemanipulated independently from each other. Insulator openings 143 a and143 b do not extend to the edge but are used to provide additionalflexibility to first harness portion 103 a as will now be explained withreference to FIGS. 16B-16F.

FIG. 16B illustrates insulator 142 comprising three insulator openings143 a-143 c that divide an insulator into four insulator strips 145a-145 d. Each strip may support a separate conductor trace (not shown)when insulator 142 is a part of a harness. It should be noted thatinsulator 142 is a part of the harness when manipulations shown in FIG.16C are performed with insulator 142.

FIG. 16C illustrates one end of insulator 142 turned 90° relative to theother end within the X-Y plane. Insulator openings 143 a-143 c allowinsulator 142 to turn and bend without significant out of planedistortions of individual insulator strips 145 a-145 d. One havingordinary skills in the art would understand that such bending would bedifficult without insulator openings because of the flat profile ofinsulator 142 (small thickness in the Z direction) and the relativelylow in-plane flexibility of materials forming insulator 142. Addinginsulator openings 143 a-143 c allows different routing of each of fourinsulator strips 145 a-145 d, thereby increasing flexibility anddecreasing the out of plane distortion. Furthermore, selecting aparticular width and length of each insulator opening allows forspecific routing and orientation of each insulator strip. FIGS. 16E and16F represent cross-sections of insulator strips 145 a-145 d atdifferent locations of insulator 142. As shown in these figures,insulator strips 145 a-145 d may be brought closer together and rotated90° around each of their respective center axes at some point (B-B) inthe bend. To achieve this type of orientation, the length of eachinsulator opening may be different or staggered as, for example, shownin FIG. 16B.

PROCESSING EXAMPLES

FIG. 17 is a process flowchart corresponding to method 1700 of formingan electrical harness or portions thereof, in accordance with someembodiments. Various examples of the electrical harness are describedabove. Method 1700 may commence with laminating a conductor to asupporting substrate during step 1710. The conductor may be a metalsheet (e.g., metal foil). Some examples of the conductor are describedbelow with reference to FIGS. 22A-22C.

Method 1700 may proceed with patterning the conductor during step 1720.One or more conductor traces are formed during this step. As describedabove, a conductor trace may include a conductor lead and a firstconnecting end. Various examples of conductor traces and theirarrangement prior to further processing is described above. Patterningthe conductor may involve techniques including, but not limited to,punching, flat bed die cutting, match-metal die cutting, male/female diecutting, rotary die cutting, laser cutting, laser ablation, waterjetcutting, machining, or etching.

Method 1700 may proceed with shaping the attachment portion of conductorduring optional step 1730. For example, individual strands may be foldedor otherwise rearranged into a shape that has a smallerwidth-to-thickness ratio than before this step as described above withreference to FIGS. 8A-10C. In some embodiments, after completing step1730, the width-to-thickness ratio of the attachment portion matches theratio of the terminal. Furthermore, step 1730 may involve stacking ofdifferent conductor traces as described above with reference to FIGS.2A-4B.

Method 1700 may proceed with attaching a connector to the attachmentportion during step 1740. For example, the connector may be crimpedand/or welded to the terminal as described above with reference to FIGS.1A-1B. In another example, a mechanical biasing attachment may be formedbetween the connector terminal and the attachment portion as describedabove with reference to FIG. 5.

In some examples, step 1740 also comprises optional step 1745 ofattaching one or more terminals to the housing of a connector. Forexample, the terminals may be inserted into the plastic housing. Anexample of the assembly formed during step 1745 is shown in FIG. 14C.

Method 1700 may proceed with attaching an insulator to the patternedconductor during step 1750. In some examples, step 1750 is performedafter step 1740. Alternatively, step 1750 is performed before step 1740.The insulator attached during step 1750 may be a permanent component ofthe electrical harness. Some examples of insulator materials areinsulator comprises a material selected from the group consisting ofpolyimide (PI), polyethylene naphthalate (PEN), polyethyleneterephthalate (PET), polymethyl methacrylate (PMMA), ethyl vinyl acetate(EVA), polyethylene (PE), polypropylene (PP), polyvinyl fluoride (PVF),polyamide (PA), soldermask, and polyvinyl butyral (PVB). Alternatively,the insulator may comprise an adhesive, such as a pressure-sensitiveadhesive, a thermoplastic adhesive, or a thermoset adhesive.

Method 1700 may proceed with unfolding the conductor traces duringoptional step 1760. Various aspects of this step are described abovewith reference to FIGS. 14A-14B and 14D-14E. Unfolding of the conductortraces may be performed before or after adding the terminals.

Method 1700 may proceed with attaching the harness to a carrier (e.g.,heat sink) during optional step 1770. For example, the carrier may be acar door as will be described below with reference to FIGS. 19A-19C.

JUMPER EXAMPLES

In some embodiments, electrical harness assembly 100 further comprisessecond conductor trace 140 b, which in turn comprises second conductorlead 150 b and second connecting end 160 b. This example isschematically shown in FIG. 18A. The thickness of second conductor trace140 b and the thickness of first conductor trace 140 a may beapproximately equal (e.g., within 10% or even within 5%, or evenidentical). For example, first conductor trace 140 a and secondconductor trace 140 b may be formed from the same foil sheet.Furthermore, first conductor lead 150 a and second conductor lead 150 bare formed from the same material. Second conductor trace 140 b andfirst conductor trace 140 a may not contact each other. For example,second conductor trace 140 b and first conductor trace 140 a may beseparated by a gap.

In some embodiments, second connecting end 160 b of second conductortrace 140 b is electrically coupled to multiple connecting portions ofconnector 110. For example, FIG. 18B illustrates second connecting end160 b being electrically coupled to five connecting portions 130 b-130 fof connector 110. As such, making an electrical connection to any one ofcorresponding contact interface 120 b-120 f will result in an electricalconnection to second connecting end 160 b. In some embodiments, themultiple connecting portions may be interconnected by one or morejumpers 170 as, for example, schematically shown in FIGS. 18B-18D.Jumpers 170 allow current balancing to be achieved within connector 110such that a relatively constant current density can be maintained acrossthe cross-section of second connecting end 160 b, thereby allowing theuse of thinner materials for second connecting end 160 b and secondconductor trace 140 b.

Second conductor trace 140 b may have a larger current carryingcapability than first conductor trace 140 a. More specifically, secondconductor trace 140 b may be wider than first conductor trace 140 a as,for example, shown in FIG. 18B. To accommodate this variation in tracewidth, connecting portions 130 a-130 f may comprise a top-down crimpconnector such as a zero-insertion force (ZIF) connector, for example.Similarly, connector 110 may be designed to accommodate wires 180 a, 180b of varying diameter, as shown in FIG. 18B-18C. Thus, connector 110 caninterconnect conductor traces 140 a, 140 b of varying width to wires 180a, 180 b of varying diameter with minimal current crowding and/or jouleheating effects in either element.

Car Doors with Flat Harnesses

FIG. 19A illustrates car door assembly 200 comprising car door 210 andelectrical harness assembly 100, in accordance with some embodiments.Electrical harness assembly 100 may be attached to and mechanicallysupported by car door 210. For example, electrical harness assembly 100,which is flat, may be adhered to car door 210. Furthermore, in thisexample, electrical harness assembly 100 may be in thermal communicationwith car door 210. More specifically, each of conductor leads 150(hidden under the insulator in FIG. 19A) of flat electrical harnessassembly 100 may be in thermal communication with car door 210. Thisthermal communication is used for heat dissipation from conductor leads150 while passing electrical currents through conductor leads 150. Morespecifically, this thermal communication allows using conductor leads150 with smaller (e.g., 30-90% smaller) cross-sectional areas than thosein conventional harnesses, which utilize round wires with minimalthermal communication to car doors or other components of a vehicle. Cardoor 210 provides a large thermal mass for heat dissipation fromconductor leads 150 when conductor leads 150 heat up while passingelectrical currents.

Electrical harness assembly 100 may comprise one or more connectors(e.g., connectors 110 a-110 c shown in FIG. 19A) for connecting toelectrical devices 220 of car door assembly 200 and outside of car doorassembly 200. Some examples of electrical devices 220 include but arenot limited to speakers, lights, door lock, window regulators, powermirrors, and the like. Connections between conductor leads 150 andconnectors 110 a-110 c of electrical harness assembly 100 are describedabove. While the above description shows that electrical harnessassembly 100 is a part of car door assembly 200, electrical harnessassembly 100 may be used for other applications as well, e.g., in whichthermal sinks are available and can be thermally coupled to electricalharness assembly 100. For example, electrical harness assembly 100 maybe used for various appliances (e.g., refrigerators, washer/driers,heating, ventilation, and air conditioning).

Reducing the cross-sectional area of conductor leads 150 corresponds toa reduction in weight of conductor leads 150. For example, many moderncars utilize 1,000-4,000 meters of electrical cables with a total weightof up to 50 kilograms and even up to 100 kilograms. Any reduction inweight helps with fuel economy, car handling, and cost savings.

Furthermore, a combination of the smaller cross-sectional area and ofthe flat profile of electrical harness assembly 100 allows a substantialreduction in the thickness of electrical harness assembly 100.Specifically, the contribution by electrical harness assembly 100 to thethickness of car door assembly 200 is reduced. As such, car doorassembly 200 may be made thinner with electrical harness assembly 100described herein than with a conventional round-wire bundled harness.

For example, comparing round wires to conductor leads 150, which areflat but have the same cross-sectional area as the round wires yet havea thickness-to-width ratio of 1:10, the reduction in thickness is about62%; i.e., the thickness of conductor leads 150 is about 38% of thethickness of round wires. Furthermore, the cross-sectional area ofconductor leads 150 may be further reduced in comparison to theconductor leads 150 due to the improved heat dissipation of conductorleads 150 to the environment, as described above. The cross-sectionalarea reduction further reduces the thickness of conductor leads 150. Theoverall thickness reduction allows increasing the interior space of acar or any other vehicle or machine. In some examples, this thicknessreduction allows feeding conductor leads 150 through smaller gaps thatmay not be suitable for feeding round wires rated for the same current.

As noted above, electrical harness assembly 100 may be attached tosurface 212 of car door 210. Furthermore, electrical harness assembly100 may follow the profile of surface 212. In other words, electricalharness assembly 100 may be substantially conformal surface 212 as, forexample, schematically shown in FIGS. 19A and 19B. More specifically,electrical harness assembly 100 may be conformal to surface 212 over atleast 50% of the area of electrical harness assembly 100 or at least 75%of the area, or even at least 50% of the area. This conformality ensuresthat all parts of electrical harness assembly 100 are in thermalcommunication with car door 210.

In some embodiments, surface 212 of car door 210 may have indent 214 toaccommodate electrical harness assembly 100 as, for example,schematically shown in FIG. 19C. The depth of indent 214 may besubstantially the same as the thickness of electrical harness assembly100 such that top surface 104 of electrical harness assembly 100 and aportion of surface 212 surrounding indent 214 are substantiallycoplanar. Alternatively, the indent may be shallower and a portion ofelectrical harness assembly 100 may protrude above the portion ofsurface 212 surrounding indent 214.

Electrical harness assembly 100 may comprise first insulator 142 andsecond insulator 144 such that conductor lead 150 is positioned betweenfirst insulator 142 and second insulator 144. FIG. 20 is a schematicillustration of first insulator 142, conductor lead 150, and secondinsulator 144 disposed on car door 210. First insulator 142 may comprisean adhesive layer that adheres electrical harness assembly 100 to cardoor 210.

In some embodiments, first insulator 142 is or comprises a thermallyconductive mounting adhesive. This adhesive may have a thermalconductivity of least about 0.2 W/mK (e.g., about 0.7 W/mK) or even atleast about 1.0 W/mK. This level of thermal conductivity may be obtainedin an inorganic particle-filled dielectric film or in a thermallyconductive PSA film, for example.

Other examples of first insulator 142 include but are not limited topolyimide (PI), polyethylene naphthalate (PEN), polyethyleneterephthalate (PET), polymethyl methacrylate (PMMA), ethyl vinyl acetate(EVA), polyethylene (PE), polypropylene (PP), polyvinyl fluoride (PVF),polyamide (PA), soldermask, or polyvinyl butyral (PVB). The compositionand thickness of first insulator 142 may be chosen to maximize heatdissipation through first insulator 142, prevent dielectric breakdown tothe surrounding environment, act as a sufficient mechanical barrier toair and moisture, and minimize distortion of features of conductor leads120. In some embodiments, the thickness and composition of firstinsulator 142 (and its corresponding adhesive layer, should one bepresent) is chosen to minimize the absorptive and reflective loss ofhigh frequency signals transmitted by the flexible circuit, as well asto provide an impedance match with interfacing electrical components.

The thickness of first insulator 142 may be between 1 micrometer and 500micrometers or, more specifically, between 10 micrometers and 125micrometers. In some embodiments, first insulator 142 includes anadhesive layer on the side facing car door 210. Some examples of theadhesive layer include, but are not limited to polyolefin adhesives,polyester adhesives, polyimide adhesives, acrylics, epoxies,cross-linking adhesives, PSAs, and/or thermoplastic adhesives.Optionally, the adhesive layer may be filled with thermally conductive,electrically insulating particles (e.g., alumina) to facilitate heattransfer through the adhesive material.

The material composition of second insulator 144 may be the same ordifferent as the material composition of first insulator 142. Forexample, first insulator 142 may be made from a material which is moreheat conductive that the material of second insulator 144. At the sametime, second insulator 144 may be made from a material that has bettermechanical properties than first insulator 142 to externally protectconductor lead 150 from damage once the harness is applied to car door210 and/or to support conductor lead 150 and other components ofelectrical harness assembly 100 before harness is applied to car door210.

The thickness of second insulator 144 may be the same or different asthe thickness of first insulator 142. For example, one of the insulators(e.g., second insulator 144) may be used as a primary structural supportand may be thicker or made from a mechanically stronger material thanthe other insulator. At the same time, first insulator 142 may bethinner to ensure heat transfer between conductor lead 150 and car door210.

First insulator 142 and second insulator 144 may be continuous sheetswithout any openings. First insulator 142 and second insulator 144 mayextend an entire length of conductor lead 150 while allowing connectingend 160 to extend beyond first insulator 142 and second insulator 144.Alternatively, in some embodiments, second insulator 144 may extendunderneath and provide support to connecting end 160 while firstinsulator 142 may leave connecting end 160 exposed, thus allowing accessto a first surface of connecting end 160. In some embodiments, firstinsulator 142 and second insulator 144 may be sealed against aninsulating enclosure of connector 110.

For purposes of this disclosure and unless otherwise stated, the term“insulator” refers to a structure having an electrical conductivity ofless than 10 S/cm. The term “conductor” refers to a structure having anelectrical conductivity of at least about 10,000 S/cm. The term “thermalconductor” refers to a structure having a thermal conductivity of atleast about 0.2 W/mK. Structures with a thermal conductivity of lessthan 0.1 W/mK may be referred to as “thermal insulators.” It should benoted that a thermal conductor may be also an electrical conductor butit does not have to be. For example, a class of electrically insulatingmaterials, such as diamond and aluminum nitride, are good thermalconductors. The materials may be used, for example, as a surfacecoating.

Electrical conductors are typically thermally conductive. The term“electro-thermal conductor” refers to a structure having an electricalconductivity of greater than 10,000 S/cm and a thermal conductivity ofgreater than 10 W/mK. The term “electrically isolated” may refer to alack of a physical connection between two electrical conductors, eitherdirectly or through one or more other electrical conductors.

Referring to FIGS. 21A and 21B, the width of gap 152 between firstconductor lead 150 a and second conductor lead 150 b may be betweenabout 100 micrometers and 3 millimeters or, more specifically, betweenabout 250 micrometers and 1 millimeter. The aspect ratio of gap 152, asdefined by the width of gap 152 divided by the conductor thickness(which is effective the depth of gap 152), may less than about 10 or,more specifically, less than about 5 or even less than about 2. Gap 152may be empty or filled with an adhesive.

First insulator 142 and, in some embodiments, second insulator 144maintain the orientation of first conductor lead 150 a and secondconductor lead 150 b relative to each other. This feature may be used tomaintain first conductor lead 150 a electrically insulated from secondconductor lead 150 b.

Examples of Sublayers of Electro-Thermal Conductors

In some embodiments, conductor trace 140 comprises base sublayer 1002and surface sublayer 1006 as, is shown in FIG. 22A, for example. Surfacesublayer 1006 may have a different composition than base sublayer 1002.First insulator 142 or second insulator 144 may be laminated oversurface sublayer 1006. More specifically, at least a portion of surfacesublayer 1006 may directly interface first insulator 142 or secondinsulator 144 (or an adhesive used for attaching first insulator 142 orsecond insulator 144 to conductor trace 140). In these examples, surfacesublayer 1006 is disposed between base sublayer 1002 and first insulator142 or second insulator 144. Surface sublayer 1006 may be specificallyselected to improve adhesion of first insulator 142 or second insulator144 to conductor trace 140, and/or other purposes as described below.

Base sublayer 1002 may comprise a metal selected from a group consistingof aluminum, titanium, nickel, copper, steel, and alloys comprisingthese metals. The material of base sublayer 1002 may be selected toachieve desired electrical and thermal conductivities of overallconductor trace 140 while maintaining minimal cost.

Surface sublayer 1006 may comprise a metal selected from the groupconsisting of tin, lead, zinc, nickel, silver, palladium, platinum,gold, indium, tungsten, molybdenum, chrome, copper, alloys thereof,organic solderability preservative (OSP), or other electricallyconductive materials. The material of surface sublayer 1006 may beselected to protect base sublayer 1002 from oxidation, improve surfaceconductivity when forming electrical and/or thermal contact to device,improve adhesion to conductor trace 140, and/or other purposes.Furthermore, in some embodiments, the addition of a coating of OSP ontop of surface sublayer 1006 may help prevent surface sublayer 1006itself from oxidizing over time.

For example, aluminum may be used for base sublayer 1002. While aluminumhas a good thermal and electrical conductivity, it forms a surface oxidewhen exposed to air. Aluminum oxide has poor electrical conductivity andmay not be desirable at the interface between conductor trace 140 and,for example, connection portion 130 of connector 110. In addition, inthe absence of a suitable surface sublayer, achieving good, uniformadhesion between the surface oxide of aluminum and many adhesive layersmay be challenging. Therefore, coating aluminum with one of tin, lead,zinc, nickel, silver, palladium, platinum, gold, indium, tungsten,molybdenum, chrome, or copper before aluminum oxide is formed mitigatesthis problem and allows using aluminum as base sublayer 1002 withoutcompromising electrical conductivity or adhesion between conductor trace140 and other components of electrical harness assembly 100.

Surface sublayer 1006 may have a thickness of between about 0.01micrometers and 10 micrometers or, more specifically, between about 0.1micrometers and 1 micrometer. For comparison, thickness of base sublayer1002 may be between about 10 micrometers and 1000 micrometers or, morespecifically, between about 100 micrometers and 500 micrometers. Assuch, base sublayer 1002 may represent at least about 90% or, morespecifically, at least about 95% or even at least about 99% of conductortrace 140 by volume.

While some of surface sublayer 1006 may be laminated to an insulator, aportion of surface sublayer 1006 may remain exposed. This portion may beused to form electrical and/or thermal contacts between conductor trace140 to other components.

In some embodiments, conductor trace 140 further comprises one or moreintermediate sublayers 1004 disposed between base sublayer 1002 andsurface sublayer 1006. Intermediate sublayer 1004 has a differentcomposition than base sublayer 1002 and surface sublayer 1006. In someembodiments, the one or more intermediate sublayers 1004 may helpprevent intermetallic formation between base sublayer 1002 and surfacesublayer 1006. For example, intermediate sublayer 1004 may comprise ametal selected from a group consisting of chromium, titanium, nickel,vanadium, zinc, and copper.

In some embodiments, conductor trace 140 may comprise rolled metal foil.In contrast to the vertical grain structure associated withelectrodeposited foil and/or plated metal, the horizontally-elongatedgrain structure of rolled metal foil may help increase the resistance tocrack propagation in conductor trace 140 under cyclical loadingconditions. This may help increase the fatigue life of electricalharness assembly 100.

In some embodiments, conductor trace 140 comprises electricallyinsulating coating 1008 forming surface 1009 of conductor trace 140opposite of device-side surface 1007 as, for example, shown in FIG. 22C.At least a portion of this surface 1009 may remain exposed in electricalharness assembly 100 and may be used for heat removal from electricalharness assembly 100. In some embodiments, the entire surface 1009remains exposed in electrical harness assembly 100. Insulating coating1008 may be selected for relatively high thermal conductivity andrelatively high electrical resistivity and may comprise a materialselected from a group consisting of silicon dioxide, silicon nitride,anodized alumina, aluminum oxide, boron nitride, aluminum nitride,diamond, and silicon carbide. Alternatively, insulating coating maycomprise a composite material such as a polymer matrix loaded withthermally conductive, electrically insulating inorganic particles.

In some embodiments, conductor trace 140 is solderable. When conductortrace 140 includes aluminum, the aluminum may be positioned as basesublayer 1002, while surface sublayer 1006 may be made from a materialhaving a melting temperature that is above the melting temperature ofthe solder. Otherwise, if surface sublayer 1006 melts during circuitbonding, oxygen may penetrate through surface sublayer 1006 and oxidizealuminum within base sublayer 1002. This in turn may reduce theconductivity at the interface of the two sublayers and potentially causea loss of mechanical adhesion. Hence, for many solders which are appliedat temperatures ranging from 150-300 C, surface sublayer 1006 may beformed from zinc, silver, palladium, platinum, copper, nickel, chrome,tungsten, molybdenum, or gold.

Multi-Harness Handling Examples

FIG. 23 illustrates an example of electrical harness assembly 100 a andelectrical harness assembly 100 b supported on the same carrier film2300. This example simplifies handling of electrical harness assembly100 a and electrical harness assembly 100 b during their production,storage, and initial application. For example, electrical connectionscan be formed to multiple conductor leads 150 a-150 d prior toseparating electrical harness assembly 100 a and electrical harnessassembly 100 b from carrier film 2300. Once electrical harness assembly100 a is removed from carrier film 2300, adhesive layer 2310 a may beused for attaching electrical harness assembly 100 a to other supportstructures (e.g., heat sinks). Cut opening 2320 may be positionedbetween electrical harness assembly 100 a and electrical harnessassembly 100 b to allow independent removal of each harness from carrierfilm 2300. In some examples, first insulator portion 142 a and firstadhesive layer 2310 a may optionally be combined into a single layer orbe separate layers. Likewise, second insulator portion 142 b and secondadhesive layer 2310 b may optionally be combined into a single layer orbe separate layers.

CONCLUSION

Although the foregoing concepts have been described in some detail forpurposes of clarity of understanding, it will be apparent that certainchanges and modifications may be practiced within the scope of theappended claims. It should be noted that there are many alternative waysof implementing the processes, systems, and apparatuses. Accordingly,the present embodiments are to be considered as illustrative and notrestrictive.

What is claimed is:
 1. An electrical harness assembly comprising: aconnector, comprising a first contact interface and a first connectingportion; and a first conductor trace, comprising a first conductor leadand a first connecting end, wherein: the first conductor lead and thefirst connecting end of the first conductor trace are monolithic; thefirst conductor lead has a width-to-thickness ratio of at least 2; andthe first connecting end of the first conductor trace is electricallycoupled to the first connecting portion of the connector.
 2. Theelectrical harness assembly of claim 1, wherein: the first connectingportion of the connector comprises a base and one or more tabs; and thefirst connecting end of the first conductor trace is crimped between thebase and the one or more tabs of the first connecting portion.
 3. Theelectrical harness assembly of claim 2, wherein the first connecting endof the first conductor trace is welded to the base.
 4. The electricalharness assembly of claim 1, wherein: the first connecting portion ofthe connector comprises a first plate and a second plate parallel to thefirst plate and forming a cavity; the first connecting portion furthercomprises a biasing element protruding into the cavity from the firstplate toward the second plate; and the first connecting end of the firstconductor trace protrudes into the cavity and contacts the biasingelement.
 5. The electrical harness assembly of claim 1, wherein thefirst connecting end of the first conductor trace has awidth-to-thickness ratio less than the width-to-thickness ratio of thefirst conductor lead.
 6. The electrical harness assembly of claim 5,wherein the first connecting end is folded.
 7. The electrical harnessassembly of claim 5, wherein the first connecting end is reshaped. 8.The electrical harness assembly of claim 5, wherein the first connectingend is slit into a plurality of strands; and wherein the plurality ofstrands is bundled together.
 9. The electrical harness assembly of claim1, further comprising a second conductor trace, comprising a secondconductor lead and a second connecting end, wherein: the secondconductor lead and the second connecting end of the second conductortrace are monolithic; the second conductor lead has a width-to-thicknessratio of at least 0.5; a thickness of the second conductor lead and athickness of the first conductor lead are equal; and the secondconductor lead and the first conductor lead do not contact each other.10. The electrical harness assembly of claim 9, wherein the secondconnecting end of the second conductor trace is electrically coupled tomultiple connecting portions of the connector.
 11. The electricalharness assembly of claim 10, wherein the connector comprises one ormore jumpers electrically coupling the multiple connecting portions. 12.The electrical harness assembly of claim 10, wherein the secondconductor lead is wider than the first conductor lead.
 13. Theelectrical harness assembly of claim 1, wherein the first connecting endis a stack of multiple layers formed by folding the first conductortrace.
 14. The electrical harness assembly of claim 13, wherein thefirst connecting end is a stack of two layers.
 15. A car door assemblycomprising: a car door comprising a surface; an electrical harnessassembly directly interfacing the surface of the car door, wherein: theelectrical harness assembly is attached to the surface of the car door;the electrical harness assembly is conformal to the surface of the cardoor; and the electrical harness assembly has a width-to-thickness ratioof at least about
 2. 16. The car door assembly of claim 15, wherein theelectrical harness assembly is attached to the surface of the car dooralong at least 90% of an interface between the electrical harnessassembly and the surface.
 17. The car door assembly of claim 15, whereinthe electrical harness assembly comprises a first insulator, a firstconductor trace, and a second insulator, wherein: the first conductortrace is disposed between the first insulator and the second insulator;and the first insulator is disposed between the first conductor traceand the surface of the car door.
 18. The car door assembly of claim 17,wherein the first insulator is adhered to the surface of the car doorusing a thermally conductive mounting adhesive.
 19. The car doorassembly of claim 18, wherein the thermally conductive mounting adhesiveis a thermally conductive pressure-sensitive adhesive (PSA) film. 20.The car door assembly of claim 17, wherein the first insulator comprisesa material selected from the group consisting of polyimide (PI),polyethylene naphthalate (PEN), polyethylene terephthalate (PET),polymethyl methacrylate (PMMA), ethyl vinyl acetate (EVA), polyethylene(PE), polypropylene (PP), polyvinyl fluoride (PVF), polyamide (PA),soldermask, and polyvinyl butyral (PVB).